Patent GB-1161918-A (GB)
Title: Improvements in or relating to Steering Gear Assemblies
IPC: B62D3/10
Filed: 1967-06-27
Abstract: 1,161,918. Cam mechanisms. TRW Inc. 27 June, 1967 [3 April, 1967], No. 29663/67. Heading F2K. In a steering gear of the kind in which a steering roller 42 is rotatably mounted in a pocket 26 formed in a cross-shaft 27, and the roller engages a worm on a steering shaft, flat thrust washers 48 are interposed between the sides of the roller 42 and the walls 28, 29 of the pocket 26. The washers 48 are prevented from rotating by the engagement of a lug 51 with milled pockets 56 in the side walls 28, 29. Each washer 48 is of soft steel and has a surface coated with sintered metallic particles, such as bronze and lead, in combination with tetrafluoroethylene. Washers 47 are located between the roller 42 and washers 48. In a modification, a washer 60 has a curved lower edge 63, Fig. 8, and is prevented from rotating by lugs 66, 67. 1,161,927. Valves. VAREC Inc. 4 April, 1967, No. 15494/67. Heading F2V. [Also in Division G3] A valve, for automatically venting a storage vessel 11 when the pressure therein is either below or above atmospheric pressure, includes a two-part valve casing 10 secured to a pipe section 12 which is welded to the vessel 11, the upper part of the casing, which is in the form of a dome 18, carrying a pressure-responsive pilot valve 34, and the lower part of the casing, formed as an open support from a series of spaced rib members 13E, being secured, together with a plate 13 having an upstanding cylindrical portion 13C, to the pipe section 12. The portion 13C constitutes a valve seat engageable by a valve closure member 20 which is carried by a diaphragm 17 secured between the two parts of the casing 10. A tapered pipe section 24 is secured to the closure member 20 and is telescopically received within a similar pipe section 32 secured to the pilot valve. In operation, upon the vessel pressure exceeding atmospheric pressure, a similar rise in pressure occurs in a chamber 26, defined by the dome 18 and diaphragm 17 and this pressure acts on the pilot valve closure member 40 tending to raise it from its seat. Upon this occurring, flow from the vessel 11 takes place through pipes 24, 32 and openings 44C to atmosphere, and flow from chamber 26 takes place through openings 38A and 44C to atmosphere, the first flow, on account of the tapered portions 24A and 32A of the pipes 24, 32, developing a velocity head which enhances exhaustion of chamber 26, serves to maintain member 40 unseated and so permits member 20 to become unseated. Upon the vessel pressure falling below atmospheric pressure, the pressure differential across the diaphragm becomes such that atmospheric pressure acting on the underside of the diaphragm raises member 20 from its seat so allowing the vessel pressure to be increased. Should the diaphragm become ruptured so preventing member 20 from unseating, then if the pressure built up in chamber 26 becomes sufficient to raise a disc-like closure member 28 from its seat, on to which it is held by a magnet 30 or spring (50, Fig. 2, not shown), a free transfer of pressure takes place through apertures 20C formed in the closure member 20.